The temperature of a flat plate is Tw = 3Te , where Te is the static temperature of the high Reynolds flow outside the boundary layer, parallel to the plate. What is the minimum value of mach number for the aerodynamic heating to become more relevant than the convective cooling for the plate?

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
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Chapter5: Analysis Of Convection Heat Transfer
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Problem 5.24P: Engine oil at 100C flows over and parallel to a flat surface at a velocity of 3 m/s. Calculate the...
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The temperature of a flat plate is Tw = 3Te , where Te is the static temperature of the high Reynolds flow outside the boundary layer, parallel to the plate. What is the minimum value of mach number for the aerodynamic heating to become more relevant than the convective cooling for the plate?
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